Prescrizione di Aeronavigabilità

Rif. N.
2014-59 del
19/feb/14
Prescrizione di Aeronavigabilità
Airworthiness Directive
Si allega la Prescrizione di Aeronavigabilità emessa dalla:
Attached the Airworthiness Directive issued by:
Agenzia Europea per la Sicurezza Aerea
European Aviation Safety Agency
Autorità Primaria di Certificazione
Primary Certification Authority
RIFERIMENTO AD
AD Reference
EASA N. 2012-0081R1
COSTRUTTORE
Manufacturer
Dassault Aviation
SOGGETTO
Applicability
Falcon 2000EX aeroplanes
OGGETTO
Subject
Airplane Flight Manual - Take-off under out-of-trim condition operational limitation
NOTE
Remark
Cancella la INFO ENAC 2012-163 del 15 maggio 2012
Nota 1
Il Certificato di Navigabilità dell'aeromobile sulle cui strutture od impianti deve essere applicata la Prescrizione
di Aeronavigabilità a riferimento, scade di validità qualora essa non venga attuata nei termini prefissati.
The Certificate of Airworthiness of the aircraft to which structures and/or systems the referenced Airworthiness
Directive shall be applied expires if the AD is not embodied within specified terms.
Nota 2
Per ulteriori informazioni contattare ENAC Direzione Regolazione Navigabilità e Operazioni
For further information contact ENAC Airworthiness and Operations Regulation Division
email : [email protected]
fax :+390644596731
EASA AD No.: 2012-0081R1
EASA
AIRWORTHINESS DIRECTIVE
AD No.: 2012-0081R1
Date: 18 February 2014
Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with
Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and
of the European third countries that participate in the activities of EASA under Article 66 of
that Regulation.
This AD is issued in accordance with EC 1702/2003, Part 21A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the
continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate
an aircraft to which an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency
[EC 2042/2003 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemption].
Design Approval Holder’s Name:
Type/Model designation(s):
DASSAULT AVIATION
Falcon 2000EX aeroplanes
TCDS Number:
EASA.A.008
Foreign AD:
Not applicable
Revision:
This AD revises EASA AD 2012-0081 dated 14 May 2012.
ATA
Airplane Flight Manual – Take-Off Under Out-Of-Trim Condition –
Operational Limitation
Manufacturer(s):
Dassault Aviation
Applicability:
Falcon 2000EX aeroplanes, all Serial Numbers (inclusive Serial Number 602)
on which Dassault Aviation modification (Mod) M2846 or Dassault Aviation
Technical Instructions TI-F2000EX-M2846-ME or TI-F2000EXM3118/M2846-ME has been embodied for the installation of winglets, except
aeroplanes that have embodied Dassault Aviation Mod M5000 or Mod M5001
in production, or have been modified in service by Dassault Aviation Service
Bulletin (SB) F2000EX-300.
Reason:
During a test flight on a Falcon 2000EX equipped with winglets (commercial
designation Falcon 2000LX), performed for the certification of a maximum
take-off weight increase, the aeroplane took off and experienced
unsatisfactory control characteristics under specific combined conditions of
loading, slat-flap setting and horizontal tailplane trim setting. The weight and
the Center of Gravity (CG) of the aeroplane during that test flight were within
the already certified limits.
This condition, if not corrected, could result in an erratic take-off path and
reduced control of the aeroplane, which could ultimately jeopardize the
aeroplane safe flight.
To address this condition, Dassault Aviation developed Change Proposal
(CP) 036 to the Airplane Flight Manual (AFM), which introduced new CG
limits which are applicable during take-off with Slat/Flap SF2 setting. Since
issuance of EASA PAD 11-077, Dassault Aviation issued a normal AFM
revision, currently at revision 15, which incorporates Dassault Aviation CP
036.
TE.CAP.00110-003 © European Aviation Safety Agency. All rights reserved.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
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EASA AD No.: 2012-0081R1
EASA issued AD 2012-0081 to require amendment of the applicable AFM to
ensure that the flight crew applies the appropriate operational procedure.
Since that AD was issued, Dassault Aviation developed Mod. M3254 and
Mod. M3457, and published Dassault Aviation SB F2000EX 300, addressing
the AFM limitations.
For the reason described above, this AD is revised to exclude new
aeroplanes variant (Dassault Aviation Mod M5000 or Mod M5001) from the
applicability and to specify that in-service modification (SB F2000EX-300)
would allow removal of the AFM amendment as required by this AD.
Effective Date:
Revision 1: 25 February 2014
Original issue: 28 May 2012
Required Action(s)
and Compliance
Time(s):
Required as indicated, unless accomplished previously:
(1) Within 14 days after 28 May 2012 [the effective date of this AD at original
issue], amend the applicable AFM to incorporate the CG limits as
indicated in sub-section 1-050-05C,1-050-05D, Weight and CG Limits of
the AFM at revision 15, and operate the aeroplane accordingly.
(2) After modification of an aeroplane in accordance with the instructions of
Dassault SB F2000EX-300, the AFM amendment as required by
paragraph (1) can be removed from the AFM of that aeroplane, provided
that concurrently to the modification, the AFM of the aeroplane is
amended to incorporate the AFM amendment applicable to the
modification, as specified in Dassault Aviation SB F2000EX-300.
Ref. Publications:
Dassault Aviation F2000EX AFM DGT88898 revision 15 dated 30 October
2011.
Dassault Aviation SB F2000EX-300 original version dated 16 April 2013,
Revision 1 dated 17 May 2013, Revision 2 dated 11 October 2013.
The use of later approved revisions of this document is acceptable for
compliance with the requirements of this AD.
Remarks:
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 27 July 2011 as PAD 11-077
for consultation until 24 August 2011. The Comment Response
Document can be found at http://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Executive Directorate, EASA. E-mail: [email protected].
4. For any question concerning the technical content of the requirements in
this AD, please contact your Dassault Falcon Technical Assistance:
- For Europe, Middle East and Africa based operators:
Hot Line: (33) 1 47 11 37 37 / Fax: (33) 1 47 11 89 49
- For USA, Canada and Mexico based operators:
Help Desk: (1) 800-2FALCON (2325266) / Fax: (1) 201 541 4740
- All other areas:
Help Desk: (1) 201 541 4747 / Fax: (1) 201 541 4740
TE.CAP.00110-003 © European Aviation Safety Agency. All rights reserved.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
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